Actuation of Bistable Laminates by Conductive Polymer Nanocomposites for use in Thermal-Mechanical Aerosurface De-icing Systems
Author:
Affiliation:
1. University of Bath
2. Massachusetts Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0105
Reference17 articles.
1. 1Gent RW., Dart NP., Cansdale JT., 2000. Aircraft Icing. Philosophical Transactions of the Royal Society A; 358: 2873-2911
2. In-Flight Icing Risk Management Through Computational Fluid Dynamics-Icing Analysis
3. Simulation of the Electroimpulse De-Icing Process of Aircraft Wings
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